CN200974500Y - Vehicle-carrying airplane - Google Patents
Vehicle-carrying airplane Download PDFInfo
- Publication number
- CN200974500Y CN200974500Y CN 200620093905 CN200620093905U CN200974500Y CN 200974500 Y CN200974500 Y CN 200974500Y CN 200620093905 CN200620093905 CN 200620093905 CN 200620093905 U CN200620093905 U CN 200620093905U CN 200974500 Y CN200974500 Y CN 200974500Y
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- CN
- China
- Prior art keywords
- aircraft
- booster
- vehicle
- wing
- telescopic boom
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Forklifts And Lifting Vehicles (AREA)
Abstract
A vehicle aircraft includes a vehicle body, a hydraulic lifting element, a telescopic boom, a windlass, a hoisting pulley, an aircraft and an aircraft booster; the device is characterized in that the vehicle body is provided with the hydraulic lifting element and the telescopic boom for the hoisting pulley to slide; the aircraft and the aircraft booster are arranged on the hoisting pulley; the body of the aircraft is provided with a telescopic element to drive the wing to flex. In the utility model, the vehicle body is provided with the hydraulic lifting element and the telescopic boom for the hoisting pulley to slide; the aircraft and the aircraft booster are arranged on the hoisting pulley; the body of the aircraft is provided with a telescopic element to drive the wing to flex; in the condition with no aircraft runway, the aircraft can reach to the position close to the enemy to achieve the sudden blow; the device solves the inadequacy of the slow speed of the existing vertical take-off and landing aircraft, and has the advantages of the good mobility and strong flexibility.
Description
Technical field
The utility model relates to the space technology field, particularly a kind of vehicle-mounted aircraft.
Background technology
Present military aircraft all needs corresponding runway and assists when taking off, in case runway is destroyed, and its operation of just can't taking off, military airfield is arranged on the rear more in addition, with the enemy army distance quite far away is arranged, so just can't implement unexpected strike, lack manoevreability and alerting ability.
Summary of the invention
The purpose of this utility model provides a kind of manoevreability and the strong vehicle-mounted aircraft of alerting ability.
The utility model is to realize like this, it comprises car body, hydraulic pressure lifting device, telescopic boom, winch, winding tackle, aircraft and aircraft booster, it is characterized in that the telescopic boom that car body is provided with hydraulic pressure lifting device and winding tackle is slided thereon, aircraft and aircraft booster are arranged on the winding tackle, are provided with to drive the flexible pipe expansion joint of wing on the body of aircraft.
The utility model is owing to be the telescopic boom that car body is provided with hydraulic pressure lifting device and winding tackle is slided thereon, aircraft and aircraft booster are arranged on the winding tackle, on the body of aircraft, be provided with and drive the flexible pipe expansion joint of wing, just can not have under the condition of airstrip, aircraft is transported to from the closer position of enemy army, implement to hit suddenly, solved the slow-footed deficiency of existing vertical take-off and landing aircraft (VTOL aircraft), have the advantage that manoevreability is good and alerting ability is strong.
Description of drawings
Below in conjunction with accompanying drawing the utility model is further described;
Fig. 1 is the structural representation of vehicle-mounted aircraft,
Fig. 2 is the structural representation of aircraft lifting,
Fig. 3 is the scheme drawing that lift-off is prepared,
Fig. 4 is the scheme drawing of boosting lift-off,
Structural representation when Fig. 5 is the aircraft wing stretching, extension,
Scheme drawing when the wing is received in Fig. 6 aircraft lift-off back,
Structural representation when Fig. 7 aircraft turns to,
Fig. 8 is the structural representation of tape guide plate aircraft when turning to.
The specific embodiment
Shown in Fig. 1-8, this vehicle-mounted aircraft comprises car body 1, hydraulic pressure lifting device 2, telescopic boom 3, flexible bracing frame 4, winch 5, winding tackle 6, aircraft 7, aircraft booster 8, fixed mount 9, retractable aircraft device 10, aircraft guide plate 11, aircraft guiding wing 12, wing 13, crane arm 14, the telescopic boom 3 that car body 1 is provided with hydraulic pressure lifting device 2 and winding tackle 6 is slided thereon, aircraft 7 and aircraft booster 8 are arranged on the winding tackle 6, on the body of aircraft 7, be provided with and drive the pipe expansion joint 10 that wing 13 stretches, its working process is at first with crane arm 14 aircraft to be lifted on the winding tackle 6, the wing 13 of aircraft 7 inwardly shrinks under the drive of retractable aircraft device 10, car body 1 carries aircraft 7 and drives towards preposition, when needs are taken off, by hydraulic pressure lifting device 2 and winch 5 telescopic boom 3 is propped and launched, lighting aircraft booster 8 launches aircraft 7, shrink wing 13 by the drive of pipe expansion joint 10 aircraft 7 lift-off backs, when aircraft need turn to, can and change aircraft guide plate 11 by pipe expansion joint 10 one-sided contraction aircraft guiding wings 12 and realize.
Claims (1)
1, a kind of vehicle-mounted aircraft, it comprises car body, hydraulic pressure lifting device, telescopic boom, winch, winding tackle, aircraft and aircraft booster, it is characterized in that the telescopic boom that car body is provided with hydraulic pressure lifting device and winding tackle is slided thereon, aircraft and aircraft booster are arranged on the winding tackle, are provided with to drive the flexible pipe expansion joint of wing on the body of aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620093905 CN200974500Y (en) | 2006-11-02 | 2006-11-02 | Vehicle-carrying airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620093905 CN200974500Y (en) | 2006-11-02 | 2006-11-02 | Vehicle-carrying airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN200974500Y true CN200974500Y (en) | 2007-11-14 |
Family
ID=38900794
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620093905 Expired - Fee Related CN200974500Y (en) | 2006-11-02 | 2006-11-02 | Vehicle-carrying airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN200974500Y (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102849221A (en) * | 2011-06-27 | 2013-01-02 | 王长存 | Short-distance lift-off vehicle for military aircraft |
| CN103802717A (en) * | 2014-01-28 | 2014-05-21 | 张中举 | Warplane highway ferry carrying platform |
| CN106892131A (en) * | 2017-03-15 | 2017-06-27 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology |
| CN106904290A (en) * | 2017-03-20 | 2017-06-30 | 余华阳 | A kind of carrier-borne aircraft power-assisted catapult launcher |
| CN108263632A (en) * | 2018-03-13 | 2018-07-10 | 江苏捷诚车载电子信息工程有限公司 | Unmanned plane transports and launch vehicle |
| CN106275391B (en) * | 2016-08-19 | 2018-10-26 | 姚立波 | The disengaged land undercarriage of aircraft |
| CN109398741A (en) * | 2018-12-12 | 2019-03-01 | 威海广泰空港设备股份有限公司 | Trailer-type unmanned plane emitter |
| CN111392057A (en) * | 2019-12-31 | 2020-07-10 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
-
2006
- 2006-11-02 CN CN 200620093905 patent/CN200974500Y/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102849221A (en) * | 2011-06-27 | 2013-01-02 | 王长存 | Short-distance lift-off vehicle for military aircraft |
| CN103802717A (en) * | 2014-01-28 | 2014-05-21 | 张中举 | Warplane highway ferry carrying platform |
| CN103802717B (en) * | 2014-01-28 | 2016-03-09 | 张中举 | Fighter plane highway transition carrying platform |
| CN106275391B (en) * | 2016-08-19 | 2018-10-26 | 姚立波 | The disengaged land undercarriage of aircraft |
| CN106892131A (en) * | 2017-03-15 | 2017-06-27 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology |
| CN106904290A (en) * | 2017-03-20 | 2017-06-30 | 余华阳 | A kind of carrier-borne aircraft power-assisted catapult launcher |
| CN108263632A (en) * | 2018-03-13 | 2018-07-10 | 江苏捷诚车载电子信息工程有限公司 | Unmanned plane transports and launch vehicle |
| CN108263632B (en) * | 2018-03-13 | 2024-03-19 | 江苏捷诚车载电子信息工程有限公司 | Unmanned aerial vehicle transportation and launching galloping |
| CN109398741A (en) * | 2018-12-12 | 2019-03-01 | 威海广泰空港设备股份有限公司 | Trailer-type unmanned plane emitter |
| CN109398741B (en) * | 2018-12-12 | 2024-03-19 | 威海广泰空港设备股份有限公司 | Trailer type unmanned aerial vehicle launching device |
| CN111392057A (en) * | 2019-12-31 | 2020-07-10 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111392057B (en) * | 2019-12-31 | 2021-06-08 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20071114 Termination date: 20091202 |